LAPSE:2023.1058
Published Article

LAPSE:2023.1058
Multimode Wind Tunnel Flow Field System Monitoring Based on KPLS
February 21, 2023
Abstract
In a wind tunnel process, Mach number is the most important parameter. However, it is difficult to measure directly, especially in the multimode operation process, leading to difficulty in process monitoring. Thus, it is necessary to measure the Mach number indirectly by utilizing data-driven methods, and based on which, to monitor the operation status of the wind tunnel process. In this paper, therefore, a multimode wind tunnel flow field system monitoring strategy is proposed. Since the wind tunnel system is a strongly nonlinear system, the kernel partial least squares method, which can efficiently handle the nonlinear regression problem, is utilized. Firstly, the Mach number is predicted utilizing the kernel partial least squares method. Secondly, process monitoring statistics, i.e., the Hotelling T2 statistic and the square prediction error, the SPE statistic, and their control limits, are proposed to be applied to monitor the wind tunnel process on the basis of the prediction of the Mach number. Finally, the Mach number prediction and monitoring strategy are applied to a real process, where mode analysis and division is necessary. After mode division, the single-mode and multimode processes are modeled and predicted, respectively, and both the single-mode and multimode processes are monitored online. Satisfactory results were achieved compared with those of the partial least squares method.
In a wind tunnel process, Mach number is the most important parameter. However, it is difficult to measure directly, especially in the multimode operation process, leading to difficulty in process monitoring. Thus, it is necessary to measure the Mach number indirectly by utilizing data-driven methods, and based on which, to monitor the operation status of the wind tunnel process. In this paper, therefore, a multimode wind tunnel flow field system monitoring strategy is proposed. Since the wind tunnel system is a strongly nonlinear system, the kernel partial least squares method, which can efficiently handle the nonlinear regression problem, is utilized. Firstly, the Mach number is predicted utilizing the kernel partial least squares method. Secondly, process monitoring statistics, i.e., the Hotelling T2 statistic and the square prediction error, the SPE statistic, and their control limits, are proposed to be applied to monitor the wind tunnel process on the basis of the prediction of the Mach number. Finally, the Mach number prediction and monitoring strategy are applied to a real process, where mode analysis and division is necessary. After mode division, the single-mode and multimode processes are modeled and predicted, respectively, and both the single-mode and multimode processes are monitored online. Satisfactory results were achieved compared with those of the partial least squares method.
Record ID
Keywords
KPLS, multimode, nonlinear, wind tunnel
Suggested Citation
Guo J, Zhang R, Cui X, Ma W, Zhao L. Multimode Wind Tunnel Flow Field System Monitoring Based on KPLS. (2023). LAPSE:2023.1058
Author Affiliations
Guo J: Aviation Technology Key Laboratory of Aerodynamics Research in High-Speed and High Reynolds, Shenyang 110819, China; Aerodynamics Research Institute, Aviation Industry Corporation of China (AVIC), Shenyang 110819, China
Zhang R: Aviation Technology Key Laboratory of Aerodynamics Research in High-Speed and High Reynolds, Shenyang 110819, China; Aerodynamics Research Institute, Aviation Industry Corporation of China (AVIC), Shenyang 110819, China
Cui X: Aviation Technology Key Laboratory of Aerodynamics Research in High-Speed and High Reynolds, Shenyang 110819, China; Aerodynamics Research Institute, Aviation Industry Corporation of China (AVIC), Shenyang 110819, China
Ma W: College of Information Science and Engineering, Northeastern University, Shenyang 110819, China
Zhao L: College of Information Science and Engineering, Northeastern University, Shenyang 110819, China [ORCID]
Zhang R: Aviation Technology Key Laboratory of Aerodynamics Research in High-Speed and High Reynolds, Shenyang 110819, China; Aerodynamics Research Institute, Aviation Industry Corporation of China (AVIC), Shenyang 110819, China
Cui X: Aviation Technology Key Laboratory of Aerodynamics Research in High-Speed and High Reynolds, Shenyang 110819, China; Aerodynamics Research Institute, Aviation Industry Corporation of China (AVIC), Shenyang 110819, China
Ma W: College of Information Science and Engineering, Northeastern University, Shenyang 110819, China
Zhao L: College of Information Science and Engineering, Northeastern University, Shenyang 110819, China [ORCID]
Journal Name
Processes
Volume
11
Issue
1
First Page
178
Year
2023
Publication Date
2023-01-06
ISSN
2227-9717
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PII: pr11010178, Publication Type: Journal Article
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LAPSE:2023.1058
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https://doi.org/10.3390/pr11010178
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Feb 21, 2023
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